文中在给出了固定增益的控制增稳系统的基本组成之后，着重介绍自动驾驶仪的参数选择特点及其对飞机飞行品质的影响。

This paper presents mainly parameter selection characteristic of autopilot and effect to flight quality of aircraft, after a basic configuration of fixed gain control augmentation system is shown.

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论述一种小型无人侦察机的飞行控制与管理系统计算机的基本设计思想。

Design principles of the flight control and managing computer of a small reconnaissance UAV are presented.

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内环路控制，对于自动驾驶仪操作，这是无关飞行航道的飞机俯仰姿态和坡度的基本控制。

INNER LOOP control, For autopilot operation this is the basis control of airplane pitch and roll attitude without regard to flight path.

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